- Registered owner
- Mustang Leasing LLC
- Location
- Henderson, NV
- Owner type
- LLC
- Serial number
- 4173
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- October 2, 2008
- Expires
- July 31, 2028
- Mode S code
- AB40D2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2002 | 1 |
|---|---|
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2008 | 3 |
| 2010 | 3 |
| 2011 | 2 |
| 2012 | 1 |
| 2013 | 4 |
| 2014 | 3 |
| 2015 | 1 |
| 2016 | 1 |
| 2017 | 3 |
| 2018 | 1 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 9 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 7 |
| 2026 | 7 |
Airframe · Eurocopter EC 130 B4
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 5
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N824MHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Eurocopter EC 130 B4 aircraft
FAA incident reports
No FAA accident or incident reports matched to N824MHMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Eurocopter EC 130 B4 aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR M7KA20110501#4173Skin · misrepairedDURING INSP A CRACK WAS DISCOVERED RADIATING FROM THE INSIDE LOWER AFT RT CORNER OF THE TAILBOOM TAIL CONE CUTOUT FOR THE HORIZ STABILIZER. AN OVER LYING SKIN DOUBLER WAS NOT CRACKED AND OBSCURED THE CRACK FROM EASY VIEWING. WITH THE HORIZ STABILIZER REMOVESDR M7KA20081219#4173Windshield · crackedWINDSCREEN FOUND CRACKED DURING PREFLIGHT INSPECTION. A NEW WINDSCREEN WAS INSTALLED. SUGGEST THAT A FORM OF REINFORCEMENT BE ADDED TO THE WINDSCREEN EDGES OR AN ALTERNATE AND MORE FLEXIBLE ADHESIVE SYSTEM BE DEVELOPED TO ALLOW FOR PLEXIGLASS EXPANSION AND CONSDR M7KA1110084173Latch · looseDURING ROUTINE INSPECTION LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. INSTALLED NEW LATCHES AS REQUIRED.SDR M7KA1017084173Latch · wornDURING ROUTINE INSP, LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. INSTALLED NEW LATCHES AS REQUIRED.SDR M7KA0701084173Turbine Blades · damagedPOWER CHECK WITH A HIGH TORQUE MARGIN AND OUT OF LIMIT T4 TEMP MARGIN WAS INDICATIVE OF TURBINE BLADE TIP DAMAGE VERIFYING DEFECT. ENGINE WAS REPLACED WITH A SERVICEABLE ASSY. THIS TURBINE RUB DEFECT HAS RECENTLY BECOME MORE PREVALENT ON THESE ENGINES. ANY CONSDR M7KA0730084173Circuit Board · failedPOSITION LIGHTS FAILED TO ILLUMINATE WITH CIRCUIT BREAKER IN CLOSED POSITION AND NO APPARENT OPENS OR SHORTS IN THE WIRE HARNESS. INVESTIGATION REVEALED THAT THE PCB TRACE FOR THE POSITION LIGHT SWITCH POWER HAD MELTED MUCH AS A FUSE BLOWS. THIS IS NOT AN UNCOSDR M7K2008F00124Exciter · failedDURING ATTEMPTED START IGNITERS FAILED TO ACTIVATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. RESETTING THE BREAKER FOR A GROUND TEST REVEALED AN UNEVEN IGNITER RHYTHM NO NORMALLY FOUND WITH THIS IGNITION SYSTEM, IGNITER BOX WAS CHANGED AS A PRECAUTSDR M7K2008F00084Exciter · failedDURING ATTEMPTED START IGNITERS FAILED TO ACTIVATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. RESETTING THE BREAKER FOR A GROUND TEST REVEALED NO FUNCTION. THIS PART HAS BEEN DEEMED NON REPAIRABLE BY THE ENGINE MFG. AS NO SECOND BOX IS EMBODIED RESDR M7K2008F00106Potentiometer · crackedAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND A FAULT CODE GENERATED INDICATING FAULT WITH COLLECTIVE LEVER VALUES BEING PROVIDED BY THE POTENTIOMETER. NEW POTENTIOMETER INSTALLED WITH NO FURTHER DEFECT NOTED. SUGGEST DIFFERENT MFG OR DESIGN BE CONSIDERED ASDR M7K2008F00105Potentiometer · defectiveAMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND A FAULT CODE GENERATED INDICATING FAULT WITH COLLECTIVE LEVER VALUES BEING PROVIDED BY THE POTENTIOMETER. NEW POTENTIOMETER INSTALLED WITH NO FURTHER DEFECT NOTED. SUGGEST DIFFERENT MFG OR DESIGN BE CONSIDERED A
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 134 STCs